Showing 8961 - 8980 out of 10430

Page 449 out of 522

Part Number Description Equivalents Action
9 PIECE EDDY CURRENT SHIM THICKNESS SET. COLOR COATED THICKNESS RANGE FROM .0005"-.010
EDDY CURRENT CIRCLE TEMPLATE, 0.750"Ø. 3 HOLE SIZES: .749", .750",.751". MATERIAL: 2024-T351, 0.063"
EDDY CURRENT CIRCLE TEMPLATE, 0.201"Ø. 3 HOLE SIZES: .200", .201",.202". MATERIAL: 2024-T351, 0.063"
EDDY CURRENT CIRCLE TEMPLATE, SELECT RIVET SIZES. 12 HOLE SIZES: .125", .156",.187", .218", .250", .281", .312", .343", .375", .437", .500", .562". MATERIAL: 2024-T351, 0.063"
EMBRAER REFERENCE STANDARD 54-50-00 PT 2 FIG 606
EMBRAER REFERENCE STANDARD 54-50-00 PT 2 FIG 615
Aeronautical Engineers Australia Reference Standard Fig.2 Page 5 DOC NO: MMS13829.001/1 and REF EO: EO13829.001/1
BOMBARDIER / CHALLENGER 604 10 STEP ALUMINUM WEDGE, ET-53-30-012 PT 6 FIG. 2 . STEP THICKNESSES:, .024", .028", .031", .035", .039", .044", .048", .052", .056" .059" +/-0.002, . PAD SIZE: 1.0" x 1.0" +/-0.010", Material: 2024-T3 ALUMINUM. Chromic anodize and 1 coat of CMS 565-01 primer on chem mill side only. Chemical mill from stock thickness 0.063” (1.60 Includes certification Report Traceable to NIST and Certificate of Conformance(COC)
BOMBARDIER / CHALLENGER 604 10 STEP ALUMINUM WEDGE, ET-53-30-012 PT 6 FIG. 2 . STEP THICKNESSES:, .024", .028", .031", .035", .039", .044", .048", .052", .056" .059" +/-0.002, . PAD SIZE: 1.0" x 1.0" +/-0.010", Material: 2124-T8 or 7075-T7 ALUMINUM. Chromic anodize and 1 coat of CMS 565-01 primer on chem mill side only. Chemical mill from stock thickness 0.063” (1.60 Includes certification Report Traceable to NIST and Certificate of Conformance(COC) Which Specifiy Conductivity Range of 35-45% IACS.
BRANTLY CALIBRATION STANDARD
BRANTLY B2 MAIN ROTOR BLADE ROOT SKIN CALIBRATION STANDARD PG.2. MATERIAL: 2024-T3 ALUMINUM BARE & CLAD. Includes Test Report and Certificate of Conformance.
CUSTOM SIKORSKY S61-N FLAT BOTTOM HOLE AFT REAR FUSELAGE REFERENCE STANDARD 51-10-05 FIGURE 7 (SHEETS 1-5). MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certiicate of Conformance.
MD REFERENCE STANDARD ETFL PROCEDURE 5 06-10-02
CUSTOM EDDY CURRENT STANDARD, 2024-T351 ALUMINUM .063"/.050". MS20426AD5 CSK RIVET 2 PLACES
REPAIR REFERENCE STANDARD GR/EP FIBERGLASS STEP DELAM DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance.
REPAIR REFERENCE STANDARD GR/EP FIBERGLASS STEP DISBOND and CORE FIBERGLASS INTERFACE. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance.
F15 REFERENCE STANDARD, 2124-T821, 1F-15A-36-2-65
F15 REFERENCE STANDARD, 2124-T821, 1F-15A-36-2-65
F15 REFERENCE STANDARD. MATERIAL: 2024-T3, OUTBOARD TORQUE BOX REAR SPAR, 68A115101, LOWER FLANGE FASTENER HOLES. Includes Test Report and Certificate of Conformance.
F15 REFERENCE STANDARD, 2124-T821, 1F-15A-36-2-65
1 446 447 448 449 450 451 452 522